[fltsim.0] JABIndex=1 title=Canada Airways Virtual ATR42-500 sim=atr42 500 model= panel=fltzip0 sound= texture= checklists= kb_checklists=checklist description=ATR42-500 v1.0 \n(c) 2001-2002 Francisco Sánchez-Castañer \nFreeware. Not for sale Repaint in Canada Airways colours by Martin Provost (c) 2002 ui_manufacturer=ATR ui_type=42 500 ui_variation=Canada Airways atc_heavy=0 atc_id= atc_airline=Canada atc_flight_number=293 [WEIGHT_AND_BALANCE] reference_datum_position=000, 0, 6.800 empty_weight_CG_position=000, 0.000, -8.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=32832.000 empty_weight_roll_MOI=260000.000 empty_weight_pitch_MOI=302000.000 empty_weight_yaw_MOI=470000.000 empty_weight_coupled_MOI=1400.000 max_gross_weight=36817.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] LeftMain=0.000, -14.500, -5.000, 758.000, 0.000 RightMain=0.000, 14.500, -5.000, 758.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=870.000 wing_span=88.750 wing_root_chord=8.830 wing_dihedral=1.500 wing_incidence=1.500 wing_twist=-1.500 oswald_efficiency_factor=0.800 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=-1.500 wing_pos_apex_vert=-8.0 htail_area=120.000 htail_span=23.917 htail_pos_lon=-36.000 htail_pos_vert=9.000 htail_incidence=0.500 htail_sweep=0.000 vtail_area=150.000 vtail_span=14.000 vtail_sweep=5.000 vtail_pos_lon=-36.000 vtail_pos_vert=9.000 elevator_area=40.000 aileron_area=35.920 rudder_area=69.530 elevator_up_limit=17.502 elevator_down_limit=10.626 aileron_up_limit=15.481 aileron_down_limit=10.897 rudder_limit=23.491 elevator_trim_limit=5.000 spoiler_limit=59.989 spoilerons_available=1 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=10.000 min_flaps_for_spoilerons=0.000 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0=1.000, 35.000, 0.000, -13.3000, 1574.803, 0.100, 0.518, 80.0, 0.150, 3.100, 0.900, 8.000, 8.000, 0.000, 0.000, 0.000 point.1=1.000, -2.0, -7.200, -13.800, 1574.803, 1.000, 0.718, 0.000, 0.283, 1.500, 0.970, 9.000, 9.000, 2.000, 0.000, 0.000 point.2=1.000, -2.0, 7.200, -13.800, 1574.803, 2.000, 0.718, 0.000, 0.283, 1.500, 0.970, 10.000, 10.000, 3.000, 0.000, 0.000 point.3=2.000, -0.500, -42.667, 3.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -0.500, 42.667, 3.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, -20.333, 0.000, -5.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 24.083, 0.000, -10.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=6.400 [GeneralEngineData] engine_type=5 Engine.0=5.900, -13.000, -8.000 Engine.1=5.900, 13.000, -8.000 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.015 inlet_area=1.000 rated_N2_rpm=21400.000 static_thrust=195.000 afterburner_available=0 [propeller] propeller_type=0 propeller_diameter=13.600 propeller_blades=6 propeller_moi=580.000 beta_max=45.000 beta_min=12.000 min_gov_rpm=16000.000 prop_tc=0.0004 gear_reduction_ratio=17.600 fixed_pitch_beta=0.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=00.000 beta_feather=86.000 power_absorbed_cf=0.900 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.000 minimum_reverse_beta=-14.000 thrust_scalar=1.208 [turboprop_engine] maximum_torque=10366.000 power_scalar=1.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [Reference Speeds] flaps_up_stall_speed=102.000 full_flaps_stall_speed=81.600 cruise_speed=304.798 [keyboard_response] elevator=30.000, 50.000 aileron=60.000, 250.000 rudder=70.000, 100.000 [Views] eyepoint=30, -1.5, -4.6 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 5.30, -38.98, -1.00, fx_navred , light.1=3, 5.30, 38.98, -1.00, fx_navgre , light.2=3, -37.30, 0.00, -4.00, fx_navwhi , light.3=2, 5.25, -38.98, -1.00, fx_strobe , light.4=2, 5.25, 38.98, -1.00, fx_strobe , light.5=1, -32.50, 0.00, 11.80, fx_beacon , light.6=1, 7.00, 0.00, -12.00, fx_beacon , light.7=4, 15, 0.00, 2, fx_vclight, light.8=4, 31.5, -2.0, -5.5, fx_vclight, light.9=4, 31.5, 2.0, -5.5, fx_vclight, [General] performance=Wing span 24.57 m \nOverall length 22.70 m \nTotal height 7.59 m \nMax. T/O weight 18600 kg \nMax. fuel weight 4500 kg \nCruising altitude 2000 - 7600 m \nCapacity payload 5750 kg \nCruising speed 472 km./h \nEngines (2) PW 127E \nMax. Power/Eng. 2400 hp \n atc_type=ATR atc_model=ATR42 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 vertical_speed_hold_available=1 [direction_indicators] direction_indicator.0=3,0 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=0.858 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=0.4 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [Flaps.0] type=1 span-outboard=0.500 extending-time=10.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=0.200 flaps-position.0=0.000, 0.000 flaps-position.1=9.998, 0.000 flaps-position.2=19.996, 0.000 flaps-position.3=29.994, 0.000 flaps-position.4=39.992, 0.000 [FlightZip] OrgPanel0=atr42-500cav\panel OrgPanInt0=